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You searched for: publisher:"Washington, D.C. : NACA"
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[texts]Correlation of supersonic convective heat-transfer coefficients from measurements of the skin temperature of a parabolic body of revolution (NACA RM-10) - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810614&ix=nu&I=0&V=D&pm=1
Keywords: Body of revolution; Aerodynamics--Research
Downloads: 67
[texts]Measurements of aerodynamic heat transfer and boundary-layer transition on a 10° cone in free flight at supersonic Mach numbers up to 5.9 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003854699&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Aerodynamics--Research
Downloads: 50
[texts]Some experiences regarding the nonlinearity of hot wires - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003760215&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Heat--Transmission
Downloads: 51
[texts]Calculation of turbulent expansion processes - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003780797&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Turbulent boundary layer
Downloads: 77
[texts]On the contribution of turbulent boundary layers to the noise inside a fuselage - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874415&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Turbulent boundary layer--Research; Airplanes--Fuselage
Downloads: 56
[texts]Exploratory investigation of transpiration cooling of a 40° double wedge using nitrogen and helium as coolants at stagnation temperatures of 1,295° to 2,910° F - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003853034&ix=nu&I=0&V=D&pm=1
Keywords: Transpiration (Physics; Aerodynamics--Research
Downloads: 42
[texts]Comparison of measured and predicted indicated angles of attack near the fuselages of a triangular-wing wind-tunnel model and a swept-wing fighter airplane in flight - Ames Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808552&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings, Triangular; Fighter planes--Wings--Testing; Aerodynamics--Research
Downloads: 68
[texts]Development of a laminar boundary layer behind a suction point - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779451&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Laminar boundary layer
Downloads: 63
[texts]experimental investigation at a Mach number of 2.01 of the effects of body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinations - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003853000&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings, Swept-back; Aerodynamics--Research
Downloads: 58
[texts]Flow past a straight- and a swept-wing-body combination and their equivalent bodies of revolution at Mach numbers near 1.0 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808476&ix=nu&I=0&V=D&pm=1
Keywords: Body of revolution; Aerodynamics--Research
Downloads: 45
[texts]Autogenous welding in airplane construction - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874350&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Airplanes--Design and construction; Oxyacetylene welding and cutting
Downloads: 217
[texts]Lame's wave functions of the ellipsoid of revolution - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003760211&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Lamé's functions
Downloads: 199
[texts]Resistance of cascade of airfoils in gas stream at subsonic velocity - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779974&ix=nu&I=0&V=D&pm=1
Keywords: Aerofoils; Aerodynamics; Laminar boundary layer
Downloads: 82
[texts]Remark on the theory of lifting surfaces - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807494&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Wings--Testing; Aerodynamics--Research
Downloads: 49
[texts]On a class of exact solutions of the equations of motion of a viscous fluid - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003770594&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Equations of motion
Downloads: 95
[texts]Correction factors for wind tunnels of elliptic section with partly open and partly closed test section - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779928&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Wind tunnels
Downloads: 170
[texts]On the representation of the stability region in oscillation problems with the aid of the Hurwitz determinants - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003771595&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Oscillations
Downloads: 168
[texts]Elasto-plastic stability of plates - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003875399&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Elastic analysis (Engineering; Axial loads
Downloads: 54
[texts]On rotational conical flow - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779475&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Rotational motion
Downloads: 146
[texts]Theoretical determination of low-drag supercavitating hydrofoils and their two-dimensional characteristics at zero cavitation number - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834476&ix=nu&I=0&V=D&pm=1
Keywords: Hydrofoils; Aerodynamics--Research
Downloads: 58
[texts]Cooling characteristics of a transpiration-cooled afterburner with a porous wall of brazed and rolled wire cloth - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808495&ix=nu&I=0&V=D&pm=1
Keywords: Afterburners--Research; Aerodynamics--Research
Downloads: 50
[texts]On the theory of the Laval nozzle - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804227&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Supersonic nozzles
Downloads: 185
[texts]Experimental investigation of the effects of viscosity on the drag of bodies of revolution at a Mach number of 1.5 - Ames Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810752&ix=nu&I=0&V=D&pm=1
Keywords: Body of revolution; Drag (Aerodynamics; Aerodynamics--Research
Downloads: 40
[texts]Experimental determination of local and mean coefficients of heat transfer for turbulent flow in pipes - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778687&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Heat--Transmission
Downloads: 167
[texts]Nonstationary gas flow in thin pipes of variable cross section - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003804176&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Difference equations; Gas flow
Downloads: 150
[texts]Effect of the acceleration of enlongated bodies of revolution upon the resistance in a compressible flow - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003759947&ix=nu&I=0&V=D&pm=1
Keywords: Body of revolution; Two-body problem; Aerodynamics; Unsteady flow (Aerodynamics
Downloads: 85
[texts]Gas flow with straight transition line - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003871226&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Gas flow
Downloads: 157
[texts]Infinitesimal conical supersonic flow - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003780782&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Differential equations
Downloads: 137
[texts]On the spectrum of natural oscillations of two-dimensional laminar flows - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874406&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Laminar flow--Research
Downloads: 134
[texts]Flat plate cascades at supersonic speed - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807842&ix=nu&I=0&V=D&pm=1
Keywords: Cascades (Fluid dynamics; Aerodynamics--Research
Downloads: 58
[texts]Investigation of Reynolds number effects for a series of cone-cylinder bodies at Mach number of 1.62, 1.93, and 2.41 - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808078&ix=nu&I=0&V=D&pm=1
Keywords: Skin friction (Aerodynamics; Aerodynamics--Research
Downloads: 78
[texts]Supersaturation in the spontaneous formation of nuclei in water vapor - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003807868&ix=nu&I=0&V=D&pm=1
Keywords: Condensation--Research; Aerodynamics--Research
Downloads: 57
[texts]Spiral motions of viscous fluids - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778985&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Viscosity solutions
Downloads: 157
[texts]On the recording of turbulent longitudinal and transverse fluctuations - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779925&ix=nu&I=0&V=D&pm=1
Keywords: Buffeting (Aerodynamics; Turbulent boundary layer
Downloads: 54
[texts]Problem of torsion in prismatic members of circular segmental cross section - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003875298&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Torsion
Downloads: 194
[texts]Heat transmission in the boundary layer - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003759949&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Turbulent boundary layer
Downloads: 93
[texts]Displacement effect of the laminar boundary layer and the pressure drag - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779843&ix=nu&I=0&V=D&pm=1
Keywords: Drag (Aerodynamics; Laminar boundary layer
Downloads: 156
[texts]Some effects of heat transfer at Mach number 2.0 at stagnation temperatures between 2,310° and 3,500° R on a magnesium fin with several leading-edge modifications - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003853254&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Aerodynamics--Research; Magnesium--Electrometallurgy
Downloads: 86
[texts]Contributions to the theory of the spreading of a free jet issuing from a nozzle - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779926&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Jet nozzles
Downloads: 52
[texts]Pressure distribution and pressure drag for a hemispherical nose at Mach numbers 2.05, 2.54, and 2.04 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003809150&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics--Research; Drag (Aerodynamics
Downloads: 166
[texts]Heat transfer and pressure measurement on a 5-inch hemispherical concave nose at a Mach number of 2.0 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003834297&ix=nu&I=0&V=D&pm=1
Keywords: Skin friction (Aerodynamics; Noses (Aircraft; Heat--Transmission
Downloads: 56
[texts]Theoretical investigation of the drag of generalized aircraft configurations in supersonic flow - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003874442&ix=nu&I=0&V=D&pm=1
Keywords: Drag (Aerodynamics; Aerodynamics, Supersonic; Airplanes--Design and construction
Downloads: 84
[texts]Experimental investigation of air-flow uniformity and pressure level on wire cloth for transpiration-cooling applications - Lewis Research Center
http://uf.catalog.fcla.edu/uf.jsp?st=UF003810536&ix=nu&I=0&V=D&pm=1
Keywords: Airplanes--Motors--Cooling; Aerodynamics--Research
Downloads: 94
[texts]Experimental convective heat transfer to a 4-inch and 6-inch hemisphere at Mach numbers from 1.62 to 3.04 - Langley Aeronautical Laboratory
http://uf.catalog.fcla.edu/uf.jsp?st=UF003808467&ix=nu&I=0&V=D&pm=1
Keywords: Heat--Transmission; Aerodynamics--Research; Turbulent boundary layer
Downloads: 81
[texts]Microstructure of turbulent flow - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003778653&ix=nu&I=0&V=D&pm=1
Keywords: Aeronautics; Turbulence
Downloads: 102
[texts]Approximate method of integration of laminar boundary layer in incompressible fluid - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003871222&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Laminar boundary layer
Downloads: 71
[texts]Extension to the cases of two dimensional and spherically symmetric flows of two particular solutions to the equations of motion governing unsteady flow in a gas - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003875517&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Airplanes--Motors; Gas flow--Research
Downloads: 61
[texts]Investigations of the boundary-layer control on a full scale swept wing with air bled off from the turbojet - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003875541&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Airplanes--Turbojet engines--Research; Airplanes--Wings, Swept-back; Boundary layer
Downloads: 168
[texts]Concerning the flow about ring-shaped cowlings of finite thickness: Part I - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003779497&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Airplanes--Motors--Cowlings
Downloads: 52
[texts]General characteristics of the flow through nozzles at near critical speeds - United States.: National Advisory Committee for Aeronautics
http://uf.catalog.fcla.edu/uf.jsp?st=UF003780314&ix=nu&I=0&V=D&pm=1
Keywords: Aerodynamics; Supersonic nozzles--Research
Downloads: 207
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